FAA Approved Supplemental Airplane Flight Manual

Transcription

Supplemental Airplane Flight Manual
Cessna 172 M & N
FAA Approved STC SA2196CE
www.airplains.com
FAA Approved
DOCUMENT NUMBER 172056
For
Cessna 172 M & N
Serial No. 17265685 to 17271034
Serial No: ________________ Reg. #: _________________
The information contained in this flight manual is FAA Approved Material, which, Along with
the FAA Approved placards and instrument markings, is applicable to the operation of the
airplane when modified in accordance with STC 2196CE, which increases the maximum
certificated takeoff weight to 2550 LBS and limits the flap travel to 30 degrees. The airplane
must previously have been modified in accordance with ATS SA4428SW which installs a
180HP Lycoming O-360 series and a fixed pitch propeller.
FAA Approved __________________________
Margaret Kline
Manager, Wichita Aircraft Certification Office
FAA Central Region
Wichita,KS
Date:___________________________
Original Date: 09/25/86
172056 | FAA APPROVED
February 3, 2012
Page 1 of 17
Cessna 172 M & N
www.airplains.com
LOG OF REVISIONS
Revision
Page
Description
Approved
Date
Orig
All
Original Issue
-
09/25/86
1
1-10
Changed Page Numbers
Revised Cover Sheet
Added Engine Models
G.M. Baker
10/02/87
G. M. Baker
07/06/88
B.L. Sorensen
3/21/90
2
1-10
3
3&4
4
All
February 3, 2012
Added M Models
Changed name to Air Plains Services,
Corp
Added O-360-A4N
Reformatted, Added Document Number,
Moved Table of Contents from Cover
Page and Included Section Applicability,
Added Propellers,
Added Fuel Consumption Chart,
Added Section 7 Handling Service And
Maintenance
Page 2 of 17
Cessna 172 M & N
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TABLE OF CONTENTS
SECTION 1: GENERAL ........................................................................................................... 4
SECTION 2: LIMITATIONS .................................................................................................... 6
SECTION 3: EMERGENCY PROCEDURES .......................................................................... 8
SECTION 4. NORMAL PROCEDURES .............................................................................. 10
SECTION 5: PERFORMANCE .............................................................................................. 12
SECTION 6: WEIGHT AND BALANCE ................................................................................. 14
SECTION 7: HANDLING, SERVICE AND MAINTENANCE.................................................. 17
February 3, 2012
Page 3 of 17
Cessna 172 M & N
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SECTION 1: GENERAL
DESCRIPTIVE DATA
ENGINE
Engine Model Number: 0-360-A2F, A3A, A4A. A4M, and A4N
Engine Type: Normally aspirated, direct drive, air cooled, horizontally opposed,
carburetor equipped, four cylinder engine with 360 cu. in. displacement.
Horsepower Rating and Engine Speed 180 rated BHP at 2700RPM.
Maximum Continuous RPM: 2700 RPM
PROPELLERS:
Sensenich Propellers approved on installations using the O-360-A4 series engines only
Propeller Manufacturer: Sensenich Corporation
Propeller Model Number: 76EM8S14-0-60
Number of Blades: 2.
Propeller Diameter: Maximum ......................................................... 76 inches.
Minimum .......................................................... 76 inches.
Pitch Range: 62” to 56 “
Propeller Manufacturer: Sensenich Corporation.
Propeller Model Number: 76EM8S-0-60 (when using MKA3.5 prop spacer).
Propeller Diameter: Maximum: .......................................................... 76 inches.
Minimum:........................................................... 76 inches.
Pitch Range: 62” to 56”
Approved on all approved engine installations:
Propeller Manufacturer: McCauley Accessory Division.
Propeller Model Number: 1A170/CFA
1A170E/CFA
Minimum:........................................................ 74.5 inches.
Propeller Type:
Fixed Pitch
Pitch Range: 60” to 56”
February 3, 2012
Page 4 of 17
Cessna 172 M & N
www.airplains.com
Approved on installations using the O-360-A4A, -A4M, -A4N, and A3A engines only:
Propeller Manufacturer: McCauley Accessory Division.
Propeller Model Number: 1A170/JFA
Minimum:........................................................ 74.5 inches.
Propeller Type: Fixed Pitch
Pitch Range:
60” to 56”
MAXIMUM CERTIFICATED WEIGHTS
Takeoff,
Landing,
February 3, 2012
Normal ..................................................................2550 lbs.
Utility ....................................................................2000 lbs.
Normal ..................................................................2550 lbs.
Utility ....................................................................2000 lbs.
Page 5 of 17
Cessna 172 M & N
www.airplains.com
SECTION 2: LIMITATIONS
AIRSPEED INDICATOR MARKINGS
Air Plains Services PN: 172861 or 172861-2 or existing airspeed indicator, marked as
follows:
MARKING
KIAS VALUE OR RANGE
White Arc .......................................................... 40-85
Green Arc ........................................................ 50-127
Yellow Arc ..................................................... 127-158
Red Line ............................................................. 158
AIRSPEED LIMITATIONS
VA
Maneuvering Speed:
2550 Pounds ........................................ 105 KIAS
2150 Pounds .......................................... 95 KIAS
1750 Pounds .......................................... 85 KIAS
POWER PLANT LIMITATIONS
Engine Model Number: O-360-A2F, A3A, A4A, A4M and A4N
Maximum Power: 180 BHP rating
Maximum Continuous RPM: 2700 RPM
Static RPM Limits: 2250 to 2450 RPM
WEIGHT LIMITS
Maximum Takeoff Weight,
Normal ........................................................2550 lbs.
Utility ...........................................................2000 lbs.
Maximum Landing Weight,
Normal ........................................................2550 lbs.
Utility ...........................................................2000 lbs.
February 3, 2012
Page 6 of 17
Cessna 172 M & N
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CENTER OF GRAVITY LIMITS –
NORMAL CATEGORY
Center of Gravity Range:
Forward: 35 inches aft of datum at 1950 lbs. or less, with straight line
variation to 41.0 inches aft of datum at 2550 lbs.
Aft:
47.3 inches aft of datum at all weights.
UTILITY CATEGORY
Center of Gravity:
Forward: 35 inches aft of datum at 1950lbs. or less, with straight line
variation to 35.5 inches aft of datum at 2000lbs.
Aft:
40.5 inches aft of datum at all weights.
FLIGHT LOAD FACTORS
NORMAL CATEGORY
Flight Load Factors (Maximum Takeoff Weight - 2550 lbs.):
Flaps Up ...................................................................... +3.8g, -1.52g
Flaps Down.............................................................................. +3.0g
PLACARDS
10 . Near airspeed indicator:
MANEUVER SPEED - 105 KIAS
February 3, 2012
Page 7 of 17
Cessna 172 M & N
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SECTION 3: EMERGENCY PROCEDURES
AIRSPEEDS FOR EMERGENCY OPERATION
Engine Failure after Takeoff:
Wing Flaps Up .................................................................. 70 KIAS
Wing Flaps Down .............................................................. 65 KIAS
Maneuvering Speed:
2550 lbs .......................................................................... 105 KIAS
2150 lbs ............................................................................ 95 KIAS
1750 lbs ............................................................................ 85 KIAS
Maximum Glide:
2550 lbs ............................................................................ 68 KIAS
2150 lbs ............................................................................ 62 KIAS
1750 lbs ............................................................................ 56 KIAS
Precautionary Landing With Engine Power ............................ 65 KIAS
Landing Without Engine Power:
Wing Flaps Up .................................................................. 70 KIAS
Wing Flaps Down .............................................................. 65 KIAS
ENGINE FAILURES
ENGINE FAILURE IMMEDIATELY AFTER TAKEOFF
1. Airspeed ................................ 70 KIAS (Flaps Up)
65 KIAS (Flaps Down)
ENGINE FAILURE DURING FLIGHT
1. Airspeed ................................................ 75 KIAS
FORCED LANDINGS
EMERGENCY LANDING WITHOUT ENGINE POWER
1. Airspeed ................................ 70 KIAS (Flaps Up)
65 KIAS (Flaps Down)
5. Wing Flaps ........................... AS REQUIRED (30° recommended)
PRECAUTIONARY LANDING WITH ENGINE POWER
2. Airspeed ................................................... 65 KIAS
5. Wing Flaps ......................... 30° (on final approach).
6. Airspeed ................................................... 65 KIAS
February 3, 2012
Page 8 of 17
Cessna 172 M & N
www.airplains.com
DITCHING
4. Wing Flaps .................................................. 20-30°
NOTE
If no power is available, approach at 70 KIAS with flaps up or at 65 KIAS with 10° flaps.
ICING
INADVERTENT ICING ENCOUNTER
11. Approach at 80 to 90 KIAS depending upon the amount of the accumulation.
February 3, 2012
Page 9 of 17
Cessna 172 M & N
www.airplains.com
SECTION 4. NORMAL PROCEDURES
NORMAL PROCEDURES
SPEEDS FOR NORMAL OPERATION
Unless otherwise noted, the following speeds are based on a maximum weight of 2550
pounds and may be used for any lesser weight.
Takeoff
Normal Climb Out .........................................................................75-85 KIAS
Short Field Takeoff, Flaps 10°, Speed at 50 Feet ............................. 57 KIAS
Enroute Climb, Flaps Up:
Normal, Sea Level ........................................................................75-85 KIAS
Normal, 10,000 Feet.....................................................................70-80 KIAS
Best Rate of Climb, Sea Level .......................................................... 73 KIAS
Best Rate of Climb, 10,000 Feet ....................................................... 72 KIAS
Best Angle of Climb, Sea Level ......................................................... 62 KIAS
Best Angle of Climb, 10,000 Feet ...................................................... 67 KIAS
Landing Approach:
Normal Approach, Flaps Up .........................................................65-75 KIAS
Normal Approach, Flaps 30° ........................................................60-70 KIAS
Short Field Approach, Flaps 30° ....................................................... 62 KIAS
Balked Landing:
Maximum Power, Flaps 20°. ............................................................. 60 KIAS
Maximum Recommended Turbulent Air Penetration Speed:
2550 Lbs ......................................................................................... 105 KIAS
2150 Lbs ........................................................................................... 95 KAIS
1750 Lbs ........................................................................................... 85 KIAS
SHORT FIELD TAKEOFF
Climb Speed
..........................................
57 KIAS (until all obstacles are cleared)
..........................................
75-85 KIAS
ENROUTE CLIMB
Airspeed
February 3, 2012
Page 10 of 17
Cessna 172 M & N
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LANDING
NORMAL LANDING
1. Airspeed ............................................. 65-75 KIAS (Flaps Up)
2. Wing Flaps ................. AS DESIRED (0-10° below 110 KIAS)
10-30° below 85 KIAS)
3. Airspeed ........................................ 60-70 KIAS (Flaps Down)
SHORT FIELD LANDING
1. Airspeed ............................................. 65-75 KIAS (Flaps Up)
2. Wing Flaps ............................................... FULL DOWN (30°)
3. Airspeed .................................................. 62 KIAS (until flare)
BALKED LANDING
5. Wing Flaps ........................... 10° (until obstacles are cleared)
RETRACT SLOWLY after reaching a safe altitude and 65 KIAS.
February 3, 2012
Page 11 of 17
Cessna 172 M & N
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SECTION 5: PERFORMANCE
LANDING DISTANCE - SHORT FIELD
CONDITIONS:
Flaps 30°
NOTES:
If a landing with flaps up is necessary, increase approach speed by 9 KIAS and allow
for 35% longer distance.
Weight
LBS
Speed
At
50 Ft
KIAS
Press
Alt
Ft
2550
62
S.L
1000
2000
3000
4000
5000
6000
7000
8000
February 3, 2012
O°C
Grnd
Roll
Ft
545
565
585
610
630
655
680
705
735
Total
Ft To
Clear
50 Ft
Obs
1290
1320
1355
1385
1425
1460
1500
1545
1585
10°C
Grnd
Roll
Ft
565
585
610
630
655
680
705
730
760
Total
Ft To
Clear
50 Ft
Obs
1320
1350
1385
1425
1460
1500
1540
1585
1630
20°C
Grnd
Roll
Ft
585
605
630
655
675
705
730
760
790
Total
Ft To
Clear
50 Ft
Obs
1350
1385
1420
1460
1495
1535
1580
1625
1670
30°C
Grnd
Roll
Ft
605
625
650
675
700
725
755
785
815
Total
Ft To
Clear
50 Ft
Obs
1380
1420
1455
1495
1535
1575
1620
1665
1715
40°C
Grnd
Roll
Ft
625
650
670
695
725
750
780
810
840
Total
Ft To
Clear
50 Ft
Obs
1415
1450
1490
1530
1570
1615
1660
1705
1755
Page 12 of 17
Cessna 172 M & N
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CRUISE FUEL CONSUMPTION
(Not FAA Approved)
Conditions:
2550 Pounds
Recommended Lean
Mixture
Press.
Alt
Feet
2000
4000
6000
8000
10,000
12,000
172056
February 3, 2012
RPM
2550
2500
2400
2300
2200
2100
2600
2500
2400
2300
2200
2100
2650
2600
2500
2400
2300
2200
2700
2600
2500
2400
2300
2200
2700
2600
2500
2400
2300
2700
2600
2500
2400
2300
20C Below
Standard Temp.

GPH
BHP
Standard
Temperature

BHP
GPH
20C Above
Standard Temp.

GPH
BHP
---
---
76
10.2
72
9.6
77
69
61
55
49
--73
65
58
52
46
--77
69
62
56
50
--73
66
59
53
47
77
69
63
57
51
69
66
60
54
48
10.3
9.2
8.3
7.5
6.8
--9.7
8.8
8.0
7.3
6.6
--10.3
9.3
8.4
7.7
7.0
--9.8
8.8
8.1
7.4
6.7
10.2
9.3
8.5
7.8
7.1
9.3
8.9
8.2
7.5
6.8
72
64
58
52
46
76
68
62
55
49
44
76
72
65
59
53
47
76
69
62
56
50
45
72
65
59
53
48
65
62
56
51
45
9.6
8.7
7.9
7.2
6.6
10.2
9.2
8.3
7.6
6.9
6.3
10.1
9.6
8.8
8.0
7.3
6.7
10.1
9.2
8.4
7.7
7.0
6.4
9.6
8.8
8.1
7.4
6.8
8.8
8.4
7.7
7.1
6.5
68
61
55
49
43
72
65
58
52
47
41
72
68
62
56
50
44
71
65
59
53
47
42
68
62
56
50
45
62
59
53
48
42
9.1
8.3
7.6
6.9
6.3
9.6
8.7
8.0
7.3
6.6
6.1
9.6
9.1
8.4
7.6
7.0
6.4
9.5
8.7
8.0
7.3
6.7
6.1
9.1
8.4
7.7
7.0
6.5
8.4
8.0
7.4
6.7
6.2
Page 13 of 17
Cessna 172 M & N
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SECTION 6: WEIGHT AND BALANCE
February 3, 2012
Page 14 of 17
February 3, 2012
Cessna 172 M & N
www.airplains.com
Page 15 of 17
February 3, 2012
Cessna 172 M & N
www.airplains.com
Page 16 of 17
Cessna 172 M & N
www.airplains.com
SECTION 7: HANDLING, SERVICE AND MAINTENANCE
To operate at the 2550 gross weight, the aircraft must be equipped with 6 or more ply tires on
both the main wheels and nose wheel on all models.
 Tire Pressure should be:
 Nose Gear ............................................... 45 psi
 Main Gear ................................................ 38 psi
February 3, 2012
Page 17 of 17

FAA Approved Supplemental Airplane Flight Manual

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